What was found
(CAN) DUAL BLEED HOT CAUTION LIGHT WHEN POWER WAS ADVANCED FOR TAKE-OFF. TAKEOFF REJECTED AT APPROXIMATELY 60 KTS. NO.2 ENGINE NACELLE PRESSURE SHUT-OFF VALVE REPLACED. NO FURTHER FAULT INDICATION ON ENGINE RUN UP.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DUAL BLEED HOT CAUTION LIGHT WHEN POWER WAS ADVANCED FOR TAKE-OFF. TAKEOFF REJECTED AT APPROXIMATELY 60 KTS. NO.2 ENGINE NACELLE PRESSURE SHUT-OFF VALVE REPLACED. NO FURTHER FAULT INDICATION ON ENGINE RUN UP.